ATLAS 5 CENTAUR DEB, 44690

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 44690 is space debris in HEO originally from a launch on Wed, 17 Oct 2018 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Loading next visibility...
Identifier
44690, 2018-079BC
Orbit
HEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2018-10-17 (8 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS 5 CENTAUR DEB
1 44690U 18079BC  26234.70837372 -.00000171  00000-0  00000-0 0  9992
2 44690  13.1164  30.8320 4405958 331.8868   9.9453  1.88489438 48352
Epoch: 2026-08-22T17:00Z
TLE epoch observation values (Epoch: 2026-08-22T17:00:03.489Z)
Latitude
-0.00005°
Longitude
164.83843°
Altitude
9,687.577 km
Speed
5.935 km/s
True Right ascension
02h 03m 28s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:57:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,504.58 km
Perigee altitude
9,108.899 km
Semi-major axis
27,684.877 km
Eccentricity
0.4406
Inclination
13.1164°
RAAN
30.832°
Arg. of periapsis
331.8868°
True anomaly
27.84536°
Mean anomaly
9.9453°
Eccentric anomaly
17.56278°
Mean motion
0.47117 °/min
Orbital period
764.05 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|